Full-Scale Firing Tests of Variable Flow Ducted Rocket Engines Employing Gap Solid Fuel Gas Generator-Reference-Cited by-同舟云学术

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Full-Scale Firing Tests of Variable Flow Ducted Rocket Engines Employing Gap Solid Fuel Gas Generator

Published:2009-08-02 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Nakayama Hisahiro,Ikegami Yoshiyuki,Yoshida Akihiko,Koori Kenji,Watanabe Kiyoyuki,Tokunaga Hidenori,Shimizu Haruo,Kanaizumi Shigeyuki

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. 1Besser, H. "History of Ducted Rocket Development at Bayern-Chemie,"AIAA-2008-5261, Proceedings of 44th AIAA/ASME/SAE/ASEEJoint PropulsionConferenceandExhibit, Hartford, CT, 2008.

2. 2Besser, H., Weinreich, H., and Kurth, G. "Fit for Mission-Design Tailoring Aspects of Throttleable Ducted Rocket Propulsion Systems,"AIAA-2008-5262, Proceedings of 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Hartford, CT,2008.

3. 3Hewitt, P. W. "Status of Ramjet Programs in the United States,"AIAA-2008-5265, Proceedings of 44th AIAA/ASME/SAE/ASEEJoint PropulsionConferenceandExhibit, Hartford, CT, 2008.

4. 4QinFei,HeGuoqiang,LiJiang,andLiuPeijin,"IntegratedFlowFieldCalculationofCombustorandInletinVariableFlow Ducted Rocket,"AIAA-2008-5172, Proceedings of 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Hartford, CT,2008.

5. 5Komai, I., and Frederick, R. A. "An Analytical Assessment for the Temperature Sensitivity of Variable-flow Gas Generators,"AIAA-1994-3196, Proceedings of 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis,IN, 1994.

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2. Study on Combustion Flow-Field of Solid Ducted Rocket with Multiple Gas Nozzles;2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE);2021-07-16

3. An LES for the Effects of Particle Size and Velocity Ratio on the Flow Structure in the Secondary Combustor;International Journal of Aeronautical and Space Sciences;2020-07-20

4. Experimental investigation of the effect of the air inlet angle and the combustion pressure in a ducted rocket combustor;Progress in Propulsion Physics – Volume 11;2019

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